Last updated: 9 July 1997, 02:00 am PST, Data Controller: Allen R. Sirota
Summary Report
Retransmit Requests
Sequence Planning Recommendations & Constraints
Sequence Execution Status
Telemetry Volume
Traverse Hazards (Detected)
Subsystem Reports
Telemetry Processing Anomalies
Press Release
Wakeup:
SEQUENCE EXECUTION STATUS:
VEHICLE STATE:
(AS OF COMMAND: 5588, Shutdown (for night-time apxs)
SCET: 7/9/97 07:18:43.034
TLST: Sol 5, 97/189 14:28:00
)
BATTERY STATE/USAGE
SUBSYSTEM STATUS:
*All data downlink on Sol INCLUDING retransmitted data.
NAVIGATION PERFORMANCE:
Constraints:
THERMAL PERFORMANCE:
COMMUNICATIONS PERFORMANCE:
Statistics
Crossover Meeting:
MOBILITY PERFORMANCE:
POWER PERFORMANCE:
Today the Sojourner Rover completed its mission success goals by taking a picture of the Lander.
Web Page Authors: Henry W. Stone and
Allen.R.Sirota All information on this site, including text and images describing the
Rover is copyright © 1997, Jet Propulsion Laboratory, California Institute of Technology and the National Aeronautics and Space Administration.
SUMMARY REPORT
RETRANSMIT REQUESTS
NONE
SEQUENCE PLANNING RECOMMENDATIONS
Proceed with Nominal Sequence Plan
Operational Constraints (For next sequence)
Operational Constraints (General)
SEQUENCE EXECUTION STATUS & VEHICLE STATE
Execution: Nominal
State: Executing
Wakeup: Alarm Clock, Sol 5, 97/189-06:58:43 LTST
Crit Errors: 5080, Accel exceeds limit
Cmds Skipped: 5567 (Image), 5081,5082,5083
Telem Anomalies: Loss of Lock
Last Command: 5588, Shutdown
Executing sequence 50520D.
Mission Phase: >Primary
Mode: Shutdown
Config: ADM Deployed on Surface
Power: Nominal
Device Status: Good
Temp (Internal): Pwr Brd at Flight Allowable
Temp (External: Ambient slightly higher than expected
Temp:(Modem): Nominal
Parameter Initial Final Parameter Initial Final
----------------------------------------------------------------
X Position (m) +3.277 +3.074 LBogey (deg) -2.72 -1.52
Y Position (m) -2.690 -2.698 RBogey (deg) -8.96 -1.12
Heading (deg) 11.5 190.7 Diff (deg) + 0.8 -0.96
Pitch (deg) -4.7 +3.5 (+ Pitch -> Front down)
Roll (deg) -7.1 +2.4 (+ Roll -> Roll to Starboard)
ADM Pos (deg) -135.68 -134.4
LFS (deg) -0.6 -41.6 RFS (deg) +1.3 +42.2
LRS (deg) -0.6 +47.4 RRS (deg) 0.0 -48.6
----------------------------------------------------------------
Total Battery Remaining (Amp*hrs)
Category Allocation Initial Final *Predicted
--------------------------------------------------------------
Operations 10 8.967 8.586 8.388
Science 10 7.500 6.500 6.5
Technology 10 10.000 10.000 10.00
--------------------------------------------------------------
Total 30 26.467 25.086 24.888
* at completion of current sequence assuming nominal execution
ADM Bumper Solar
UL UR B RB LB LR RR RF LF
Mask 1 1 1 1 1 1 1 1 1
State 0 1 0 0 0 0 0 0 0
ERROR FLAGS
Skip GenFail InvalidCmd WEB_Hot NoPwr NonTrav DevNA DevFail Timeout
Mask 1 1 1 1 1 1 1 1 1
State 0 0 0 0 0 0 0 0 0
S/S Status Comments
C&N Nominal None
MTM Nominal None
Thermal Off-Nominal Power Board slightly above flight allowables.
Power Nominal None
Telecom Nominal Rover/Lander Link Good Today
TRAVERSE HAZARDS (DETECTED)
5080 move ( 3036,-2703) 0129: AY2
5080 move ( 3052,-2703) 01F6: AY2
5080 move ( 3063,-2703) 025C: AY1 AZ1
5080 move ( 3079,-2703) 03EE: AY1
5087 turn_by ( 3079,-2703) 07BA: AY2
5111 turn_at ( 3079,-2703) 0FDE: AZ1
5111 turn_at ( 3079,-2703) 3472: AZ1
5111 turn_at ( 3079,-2703) 49CF: AZ1
5111 turn_at ( 3079,-2703) 4C9E: AZ1
5557 deploy_apxs ( 3074,-2698) 87A3: AZ2
5557 deploy_apxs ( 3074,-2698) 87A3: AZ2
TELEMETRY VOLUME
DATA VOLUME SUMMARY (BY APID)*
APID #PKTS #BYTES #Mbits
----------------------------------
4 45 13235 0.10588
5 169 10341 0.08273
6 20 1200 0.00960
7 1 52 0.00042
8 586 1094250 8.75400
9 0 0 0.00000
10 0 0 0.00000
12 10 10700 0.08560
23 0 0 0.00000
24 0 0 0.00000
25 406 777388 6.21910
29 6 2878 0.02302
----------------------------------
1243 1910044 15.28035
SUBSYSTEM REPORTS
C&N subsystem components essentially all performing as expected:
Thermal subsystem components all performing as nominally
The Rover Telecom Subsystem performed nominally during the operations for SOL5.
The Rover radio modem and LMRE radio modem can be used without restriction
for upcoming sequences.
Mobility subsystem components all performing as expected.
Power subsystem components all performing as expected.
TELEMETRY PROCESSING ANOMALIES
PRESS RELEASE